(7) If you will install the same rudder trim actuator (3), do the subsequent steps:
 (a)
 Make sure that the mobile red index is in the zero position on the position indicator of the rudder trim actuator. (Ref. Fig. 405/TASK 27-22-51-991-007)

 (b)
 Cut, remove and discard the lockwire from the plug in the rigging hole of the rudder trim actuator (3).

 (c)
 Remove the plug from the rigging hole of the rudder trim actuator (3).

 (d)
 Install the PIN - LOCKING (6137-060) (19) in the rigging hole of the rudder trim actuator (3).

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 INTENTIONALLY BLANK

R 1 1

27-22-51Page 414
1 1 May 01/03 1 1 1CES 1

R Position Indicator of the Rudder Trim Actuator - PN 6137-4/6137-5 Figure 405/TASK 27-22-51-991-007
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 Installation of the Rudder Trim Actuator (10CC)
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
 START A TASK ON OR NEAR:

 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS

 -COMPONENTS THAT MOVE.
 WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______
 CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.

 WARNING : PRESSURIZE ONLY THE HYDRAULIC SYSTEM(S) THAT IS (ARE) NECESSARY FOR
_______ THE TASK. ISOLATE THE OTHER HYDRAULIC SYSTEM(S) BEFORE YOU SUPPLY HYDRAULIC POWER TO THE AIRCRAFT.
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific 2 ACCESS PLATFORM 6M (20 FT) - ADJUSTABLE
 No specific 2 WARNING NOTICE R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
 No specific Torque Wrench : range 0.20 to 3.60 m.daN
 (2.00 to 26.00 lbf.ft) 6137-013 1 PIN - LOCKING 6137-060 1 PIN - LOCKING 98D27207546000 1 PIN - RIGGING 98D27207547000 1 PIN - RIGGING 98D27207548000 1 PIN - RIGGING B. Consumable Materials

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-004  USA MIL-PRF-23827 TYPE I
 SYNTH.ESTER BASED GREASE HIGH PRESSURE
 Material No. 05-002  (Ref. 20-31-00)USA MIL-P-8116
 Material No. 19-010  PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)USA AMS 5687
 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
 (Ref. 20-31-00)

 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-912-004 22-96-00-710-001 22-97-00-710-001 24-41-00-862-002  Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-Operational Test of the AFSOperational Test of the LAND CAT III CapabilityDe-energize the Aircraft Electrical Circuits Supplied from the External Power
 27-21-00-840-001  Removal/Installation of the control rod on the rudder mechanical control
 27-22-00-710-002 27-24-00-710-001 29-00-00-864-001 55-33-13-000-001  Operational Test of the Rudder Trim ActuationOperational Test of the Rudder Hydraulic ActuationPut the Related Hydraulic System in the Depressurized Configuration before Maintenance ActionRemoval of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR
 55-33-13-010-002  Opening/Removal of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and
 325BR
 55-33-13-400-001  Installation of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and
 325BR
 55-33-13-410-002  Closing/Installation of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL,
 325CR, 325BL and 325BR
 27-22-51-991-001 27-22-51-991-004  Fig. 401Fig. 402

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 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
　
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